737 Hydraulics Flashcards

1
Q

How many hydraulic systems are there?

A

3

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2
Q

What are the hydraulic systems called?

A

A, B, Standby

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3
Q

What is the normal hydraulic pressure range?

A

3000 psi +/- 200 psi, max 3500

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4
Q

What is the purpose of the PTU? When would it operate?

A

Provide Hydraulic System B pressure sufficient to provide normal rates of operation for the Autoslats and Leading Edge Devices (LED) in the event the Hydraulic System B Engine-Driven Pump output pressure drops

Failure of Sys B

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5
Q

Are there flight deck indications of PTU operation?

A

NO

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6
Q

What are components specific to the Hydraulic System A?

A

Ailerons, Rudder, Elevator and Elevator Feel, Flight Spoilers (Two on Each Wing), Ground Spoilers, Alternate Brakes, No. 1 Thrust Reverser, Autopilot A, Normal NWS, Landing Gear, Power Transfer Unit (PTU) A for lAnding gear

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7
Q

What are components specific to the Hydraulic System B?

A

Ailerons, Rudder, Elevator and Elevator Feel, Flight Spoilers (Two on Each Wing), Leading Edge Flaps and Slats, Normal Brakes, No. 2 Thrust Reverser, Autopilot B, Alternate NWS, Landing Gear Transfer Unit (LGTU), Autoslats, Yaw Damper, Trailing Edge Flaps) B for Brakes and flaps and yaw damper

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8
Q

What does positioning a FLT CONTROL switch to STBY RUD do? looking for the logic

A

Activates the Standby Hydraulic Pump

Deactivates FLT CONTROL low pressure light Arms STBY hydraulic low pressure light

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9
Q

What is the light logic when this occurs?

A

Illuminates STBY RUD ON, FLT CONT annunciator, and MASTER CAUTION lights

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10
Q

What would cause the automatic operation of the Standby Hydraulic System?

A

Loss of A and/or B with flaps extended with wheel speed greater than 60 kts Loss of A and/or B with flaps extended airborne OR: The Force Flight Monitor (FFM) trips STBY SYSTEM -rudder -thrust reversers UNLESS you arm the Alternate Flaps and put the LE devices down

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11
Q

During normal operations, what could cause variations in hydraulic quantity indications?

A

High demand on the system

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12
Q

What would indicate a hydraulic system requires a refill? When would you see this annunciation, and where is it located?

A

Quantity below 76%, will show 30 seconds of flaps retracted on the ground.

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13
Q

What pressurizes the Hydraulic System A & B reservoirs?

A

Regulated bleed air

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14
Q

Which hydraulic reservoirs have a standpipe?

A

A and B

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15
Q

What quantity percentage do the associated standpipe(s) protect the reservoir(s) down to?

A

A - 20% enough to protect electric pump

B - 0% but enough for PTU ops only

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16
Q

With zero indicated on the Hydraulic System B quantity indicator, can the PTU still operate?

A

Yes

17
Q

When is the Standby HYD LOW QUANTITY (amber) light armed?When would it illuminate?

A

When the standby reservoir is below 50%

18
Q

What does a LOW PRESSURE (amber) light indicate? OVERHEAT (amber) light?

A

LOW PRESSURE = indicate the respective pump output pressure is low.
OVERHEAT = an overheat condition is detected in the respective system.

19
Q

Does the Hydraulic System A reservoir standpipe protect against a leak in both the engine driven pump and electric motor-driven pump? System B?

A

System A: If a leak develops in the Engine Driven Pump, the Electric Driven Pump is still available by the Standpipe, providing 20%.
If a leak develops in the Electric Driven Pump, you lose both pumps and hydraulic drops to 0%.
System B: No. Loss of both Engine and Electric Driven Pumps from a leak anywhere in the system.

20
Q

What indications, if any, would you see in the event of a Standby Hydraulic system leak?Does it affect any other system?

A

System B would decrease to 70%, affects system B

21
Q

Should both ELEC hydraulic pump switches be turned on simultaneously?
Precautions?

A

No, too much of an electrical load. #1 then #2

Need 1675 fuel in each tank for cooling

22
Q

*T/F? In System B: Extension of the Leading Edge Devices may result in up to 20% drop in hydraulic fluid quantity

A

TRUE